Airbus H225 Super Puma vs. Mil Mi-26

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Airbus H225 Super Puma versus Mil Mi-26
14.06 m 46 ft 2 in length 40.03 m 131.3 ft
4.38 m 14 ft 4 in height 8.15 m 26.7 ft
wingspan
2 x Turbomeca Makila 2A turboshaft engines engines 2 x Lotarev D-136 turboshaft engines
2,778 hp thrust per engine 8,380 kW
5,556 hp total thrust 16,760 kW
11,000 kg 24,251 lb MTOW 56,000 kg 123,459 lb
857 km 463 nm range 800 km 432 nm
242 km/h 150 mph cruise speed 255 km/h 158 mph
24-28 capacity Up to 90 passengers
16.2 m 53 ft 2 in rotor diameter 32.00 m 105 ft 0 in
10.7 m/s 2,106 ft/min rate of climb 8 m/s 1,574 ft/min
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.